SOME CONSIDERATIONS OF DIRECT‐LIFT V/STOL AIRCRAFT

Abstract

Annals of the New York Academy of SciencesVolume 107, Issue 1 p. 380-408 SOME CONSIDERATIONS OF DIRECT-LIFT V/STOL AIRCRAFT E. F. Katzenberger, E. F. Katzenberger Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this authorH. D. Ulisnik, H. D. Ulisnik Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this authorA. Adler, A. Adler Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this author E. F. Katzenberger, E. F. Katzenberger Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this authorH. D. Ulisnik, H. D. Ulisnik Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this authorA. Adler, A. Adler Sikorsky Aircraft Division, United Aircraft Corporation, Stratford, Conn, and United Aircraft Research Laboratories, E. Hartford, Conn.Search for more papers by this author First published: March 1963 https://doi.org/10.1111/j.1749-6632.1963.tb13288.xAboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onFacebookTwitterLinkedInRedditWechat Volume107, Issue1Verticle Take‐Off and Landing (VTOL) AircraftMarch 1963Pages 380-408 RelatedInformation